A combined composite and metal hybrid component 21, and a method of forming said component, comprising a substantially sheet-like or web-like planar body portion 210, made of a composite material, at least one stiffening member 211, 213, 215, 217 made of a generally rigid material particularly metal and at least one stiffening member 212, 214, 216 made of a composite material, and co-curing the component in a vacuum bag, such that the metal stiffening member is formed against the composite stiffening member and the metal stiffening member remains a part of the hybrid composite component. The method is particularly suitable for bonding fuselage or wing skins to stiffening members.
Composite structures
09.11.2016
Patent
Elektronische Ressource
Englisch
IPC: | B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B29D PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE , Herstellen besonderer Gegenstände aus Kunststoff oder aus Stoffen in plastischem Zustand |
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